(SAL) 25.4 Climb: One-engine-inoperative

• ED Decision 2013/010/R found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

(SAL) 25.4 Climb: One-engine-inoperative ED Decision 2013/010/R In a configuration corresponding to the normal all-engines-operating procedure in which VSR for this configuration does not exceed 110 % of the VSR for the related all-engines-operating steep approach landing configuration, the steady gradient of climb may not be less than 2.1 % for two-engined aeroplanes, 2.4 % for three-engined aeroplanes, and 2.7 % for four-engined aeroplanes, with: (a) The critical engine inoperative, the remaining engines at the go-around power or thrust setting; (b) The maximum landing weight; (c) A climb speed of VREF(SAL); and (d) The landing gear retracted. [Amdt 25/13]